Abstract: A craft capable of a vertical take-off and landing configuration and a horizontal thrust configuration may include, for example, at least a proprotor, an edgewise blade, and a body. The proprotor may be configured to tilt to achieve a horizontal thrust component. A portion of a lift surface may be configured to tilt with the proprotor. In some embodiments, the vertical take-off and/or landing craft may further comprise a tail connected to a first boom and a second boom. In some embodiments, the vertical take-off and/or landing craft may further comprise a tail attached to the body. In some embodiments, the craft includes four rotors positioned on the lift surface and two rotors positioned on a tail connected to the lift surface.

Abstract: A craft capable of a vertical take-off and landing configuration and a horizontal thrust configuration may include, for example, at least a proprotor, an edgewise blade, and a body. The proprotor may be configured to tilt to achieve a horizontal thrust component. A portion of a lift surface may be configured to tilt with the proprotor. In some embodiments, the vertical take-off and/or landing craft may further comprise a tail connected to a first boom and a second boom. In some embodiments, the vertical take-off and/or landing craft may further comprise a tail attached to the body.

Abstract: A drive unit for a power tool that includes a motor and a blower assembly. The motor includes a rotor shaft, a stator, and a rotor. The rotor shaft extends along an axis of rotation. The stator is mounted to the rotor shaft. The rotor at least partially surrounds the stator. The rotor has a rotor core, a plurality of magnets, and an overmold housing that couples the plurality of magnets to the rotor core to form poles having more than one magnet per pole. The blower assembly includes a plurality of blower fan blades. The blower assembly is configured to be driven by the motor.

Abstract: An aircraft comprises a fuselage, wings connected to the fuselage, engines connected to the wings, and liquid hydrogen tanks. Each engine in the engines comprises a nacelle, an electric motor within the nacelle, a fuel cell stack within the nacelle, and a nacelle heat exchanger within the nacelle that receives air flowing through an inlet in the nacelle. The liquid hydrogen tanks are configured to store liquid hydrogen, wherein the liquid hydrogen tanks extend along an outside of the fuselage and above the wings and below windows in the fuselage.

Abstract: According to some embodiments of the present disclosure, there is provided a first connector configured to be connected to an electrical cable, the first connector including an electrical connector configured to mate with and electrically connect to the electrical cable, and a body having a first end carrying a plurality of electrical terminals and having a second end coupled to an end of the electrical connector, the body including a sleeve extending from the first end to the second end, the sleeve being molded over and extending around the end of the electrical connector, and a flange axially extending outwardly from the first end of the body.

Abstract: A craft capable of a vertical take-off and landing configuration and a horizontal thrust configuration may include, for example, at least a proprotor, an edgewise blade, and a body. The proprotor may be configured to tilt to achieve a horizontal thrust component. A portion of a lift surface may be configured to tilt with the proprotor. In some embodiments, the vertical take-off and/or landing craft may further comprise a tail connected to a first boom and a second boom. In some embodiments, the vertical take-off and/or landing craft may further comprise a tail attached to the body. In some embodiments, the craft includes four rotors positioned on the lift surface and two rotors positioned on a tail connected to the lift surface.

Abstract: According to some embodiments of the present disclosure, there is provided a first connector configured to be connected to an electrical cable, the first connector including an electrical connector configured to mate with and electrically connect to the electrical cable, and a body having a first end carrying a plurality of electrical terminals and having a second end coupled to an end of the electrical connector, the body including a sleeve extending from the first end to the second end, the sleeve being molded over and extending around the end of the electrical connector, and a flange axially extending outwardly from the first end of the body.

Abstract: An apparatus including a thrust vectoring system including a centrifugal fan and a nozzle configured to output an exhaust from the centrifugal fan, wherein the thrust vectoring system is configured to controllably orient at least one of, the centrifugal fan or the nozzle, to vector a thrust generated by the exhaust.

Abstract: An apparatus including a thrust vectoring system including a centrifugal fan and a nozzle configured to output an exhaust from the centrifugal fan, wherein the thrust vectoring system is configured to controllably orient at least one of, the centrifugal fan or the nozzle, to vector a thrust generated by the exhaust.

Abstract: Split-tiltwing aircraft and related methods. The aircraft comprise a wing assembly comprising a forward wing segment and a rear wing segment. The wing assembly is configured to be transitioned among a forward thrust configuration, in which the forward and rear wing segments define a continuous airfoil shape, and a plurality of pitched thrust configurations, in which the forward and rear wing segments are spaced apart. The forward wing segment is configured to be tilted among a forward thrust position and a plurality of pitched positions. The methods comprise controlling elevation of the aircraft by controlling vectored thrust from propulsion units, and transitioning the aircraft to a cruise configuration by tilting the forward wing segment from a pitched position to a forward thrust position, in which the forward and rear wing segments define the continuous airfoil shape, and supplying forward vectored thrust to the aircraft with the propulsion units.

Abstract: A stand-alone, rigid lacrosse pocket is formed from a piece of mesh netting that is shaped to exhibit a desired pocket contour. Once shaped, a coating of stiffening material is applied to the netting and embeds within the shaped mesh netting to “fix” the desired pocket contour and form a rigid lacrosse pocket. The rigid lacrosse pocket is thereafter attached to a conventional lacrosse head, using the same stringing technique as commonly used to attach the mesh netting to the head. Advantageously, by pre-fabricating the lacrosse pocket, the need to “work” the netting into the desired shape is eliminated, and a player can quickly and easily change pockets as necessary. A method of fabricating the stand-along, rigid lacrosse pocket is also disclosed.

Abstract: A method for creating and displaying points of interest in video test results comprises obtaining a plurality of video test results, each of the plurality of video test results corresponding to a tester, and for each of the plurality of video test results, displaying the video test results, receiving at least one indicator of a point of interest in the video test results, receiving a text comment associated with the point of interest, and saving a timestamp that indicates a position in the video test results of the point of interest and a text comment in a memory. Then a graphical user interface is created that displays the timestamp and text comment of each point of interest in the plurality of test video results, where selection of a point of interest causes the corresponding video test result to be displayed beginning at the timestamp of the selected point of interest.

Abstract: One embodiment of a method for creating composite video test results includes obtaining a screenshot video of a test display, obtaining a camera video of a tester interacting with the test display, and dividing the screenshot video and camera video into segments. A plurality of composite video segments are then created, where each composite video segment is a composite of one of the plurality of camera video segments and one of the plurality of screenshot video segments. The plurality of composite video segments are then combined into a composite video. In one embodiment, audio data of the tester is combined with the composite video to create a composite audiovisual file. The composite video may be played back by a web browser in such a way that a viewer perceives the composite video as two separate videos that are synchronized.

Abstract: A control panel for a communications system of an aircraft has at least one transmitter and at least one receiver, with multiple transmission and reception channels, and multiple operating elements that have an on/off function, in each instance. Each operating element is assigned to one of the transmission and reception channels. Reception on the transmission and reception channel, in each instance, can be released by the on/off function. A selection switch has a selection position for each transmission and reception channel, in which it releases the related transmission and reception channel for the transmission and blocks the other transmission and reception channels for transmission. The selection switch has a further selection position, in which it releases the transmission and reception channels that are released for reception by the operating elements, for transmission, and blocks the other transmission and reception channels for transmission.

Abstract: A method of producing a composite part having a multicoloured surface and to a composite part having a multicoloured surface. The method contains the steps: (a) producing a multicoloured plastic film which has a groove in the area of the coloured regions adjacent to one another, (b) positioning the plastic film in a cavity of a tool, (c) partly drawing in the film regions lying along the groove into the interior of the cavity of the tool with the film regions drawn into the interior of the cavity simultaneously or subsequently being brought together for closing a recess, produced by the partial drawing-in of the film, between the film and the surface of the tool, (d) back foaming and/or back moulding the film. The method allows composite parts to be produced with a neater parting line between the individual coloured regions.

Abstract: A method by which a sponsor (24) audits convention registrants attending an event who occupy rooms at hotels (26a-26D) that the registrant does not book through the sponsor's housing provider (32). Before the event, the sponsor (24) arranges a commitment from hotels (26A-26D) for a block of rooms during the event. The auditing method includes producing an out-of-block list (64) that identifies registrants who do not appear in an in-block list (56). The out-of-block list (64) is stored on a housing-audit computer (52) from which the hotels (26A-26D) download copies. The hotels (26A-26D) in producing a match list (82) find matches between their guest list (76) and the downloaded copy of the out-of-block list (64). After validating and accepting matches between the lists (64, 76), the hotels (26A-26D) upload the match list (84) to the housing-audit computer (52) for use in producing audit reports (88) supplied to the sponsor (24).

Abstract: A system and method to promote the consumption of one or more sponsored products or brands of products within an establishment. The system provides and integrated system to track the consumption of sponsored products, control the various entertainment devices in the establishment, and to interact with customers. The system promotes the consumption of one or more sponsored products by rewarding the consumption of sponsored products with prizes, gifts, and opportunities to participate in games of chance.